SISTEMA REDUNDANTE DE RESFRIAMENTO PARA AERONAVES PARA COMPONENTES REDUNDANTES DE AERONAVE

摘要

The system (1) has a coolant stream (4a) cooling a heat load (2a), and another coolant stream (4b) cooling another heat load (2b), where the loads are generated by two mutually redundant aircraft components. The loads are bidirectionally and thermally coupled to each other. A third coolant stream (12) thermally couples the loads together and is cooled by a heat exchanger (16) e.g. aircraft's air conditioning system. An independent claim is also included for a method for cooling aircraft components.